# Service difficulty reports: N282WA, cancelled Mar 10, 2017

A list on [N282WA, cancelled Mar 10, 2017](https://openairdocs.org/deregistered/N282WA-2017-03-10.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 68 reports

- [SDR DL72E020009](https://openairdocs.org/sdr/DL72E020009.md): Battery Pack · discharged · Jan 3, 2002 · N282WA · Boeing 727247 · Emergency Lighting
  > ON LAYOVER, RT OVERWING EMERGENCY LIGHT CENTER POSITION FLICKERING. REPLACED BATTERY PACK.
- [SDR DL72E020008](https://openairdocs.org/sdr/DL72E020008.md): Power Supply · discharged · Jan 3, 2002 · N282WA · Boeing 727247 · Emergency Lighting
  > ON LAYOVER, EMERGENCY LIGHTS FROM 27 AFT INOP INCLUDING 3 EXIT LIGHTS IN AFT CABIN. REPLACED POWER SUPPLY.
- [SDR DL72E011860](https://openairdocs.org/sdr/DL72E011860.md): Charger · inoperative · Nov 25, 2001 · N282WA · Boeing 727247 · Emergency Lighting
  > FOUND ON S/C THAT FWD OVERWING LIGHTS WERE INOP.REPLACED BATTERY PACK AND CHARGER.
- [SDR DL72E011334](https://openairdocs.org/sdr/DL72E011334.md): Control Valve · failed · Aug 14, 2001 · N282WA · Boeing 727247 · Turbine Engine Compressor Section
  > EXPERIENCED COMPRESSOR STALL ON NR 2 ENGINE AT 20 KTS ON TAKEOFF ROLL. ABORTED TAKE OFF. REPLACED NR 2 PRBC.
- [SDR DL72E011317](https://openairdocs.org/sdr/DL72E011317.md): Light · inoperative · Aug 10, 2001 · N282WA · Boeing 727247 · Emergency Lighting
  > DURING LAYOVER CHECK FOUND EMERGENCY EXIT LIGHT ASSY AT AFT AIRSTAIRS INOP. WOULD NOT ILLUMINATE DURING EMERGENCY LIGHT CHECK, OR WHEN TEST SWITCH MOVED FROM ARM TO ON. REPLACED LIGHT ASSY AND BATTERIES. OPERATIONAL CHECKS NORMAL
- [SDR DL72E011105](https://openairdocs.org/sdr/DL72E011105.md): Beam · cracked · Jul 2, 2001 · N282WA · Boeing 727247 · Fuselage Main, Structure
  > INSPECTION OF THE RT TORQUE BOX OF THE VENTRAL STAIRWAY OPENING PER AD 94-07-08 AND BAC SB 727-53-0129 REVEALED A.5 INCH LONG CRACK IN THE UPPER HORIZONTAL BEAM AT FS 1263. THE DAMAGED PART WAS REMOVED AND A NEW PART INSTALLED PER THE REQUIREMENTS OF THE SB
- [SDR DL72E010641](https://openairdocs.org/sdr/DL72E010641.md): Start Valve · malfunctioned · Apr 18, 2001 · N282WA · Boeing 727247 · Engine Start Valves/Controls
  > AT CRUISE THE NR 1 ENG START VALVE ILLUMINATED. FOLLOWED THE POM AND SHUT DOWN ENGINE. OIL PRESSURE AT 37 PSI FOR 1 HOUR AND 10 MINUTES. REPLACED NR 1 ENG. START VALVE AND PRESSURE SWITCH RAN ENG. CK NORMAL. PERFORMED WINDMILLING INSPECTION PER M/M.
- [SDR DL72E010529](https://openairdocs.org/sdr/DL72E010529.md): Battery Pack · discharged · Apr 1, 2001 · N282WA · Boeing 727247 · Emergency Lighting
  > FOUND AFT EMERGENCY EXIT BATTERY DEAD. REPLACED BATTERY PACK.
- [SDR DL72E010148](https://openairdocs.org/sdr/DL72E010148.md): Compressor · stalled · Jan 26, 2001 · N282WA · Boeing 727247 · Turbine Engine Compressor Section
  > NR 1 ENGINE COMPRESSOR STALLED AT 80 KNOTS ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. ENGINE CHANGED.
- [SDR DL72E001406](https://openairdocs.org/sdr/DL72E001406.md): Battery Pack · discharged · Jul 24, 2000 · N282WA · Boeing 727247 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT AT SEAT ROW 3 INOP. REPLACED BATTERY PACK AND RACK. OPS CHECK OK.
- [SDR DL72E000303](https://openairdocs.org/sdr/DL72E000303.md): Hinge · noisey · Feb 13, 2000 · N282WA · Boeing 727247 · Passenger/Crew Doors
  > UPON LEVELING FL 260 LOUD PIERCING SQUEAL FROM FWD ENTRY DOOR. RAISED CABIN ALTITUDE, LOWERED CABIN ALT, CLIMBED A/C AND DESCENDED A/C. CABIN 5600 TO 1000 FT. A/C FL310 TO FL240. NO IMPROVEMENT. SQUEAL REMAINED. FOUND UPPER HINGE SEAL OUT OF PLACE. INST
- [SDR DL72E992493](https://openairdocs.org/sdr/DL72E992493.md): Skin · worn · Oct 26, 1999 · N282WA · Boeing 727247 · Trailing Edge Flaps
  > COVE SKIN WORN 34 FROM INBD END, REPAIRED PER MM 57-52-0 FIG 809, ON SHOP ORDER 877885.
- [SDR DL72E992202](https://openairdocs.org/sdr/DL72E992202.md): Spar · misdrilled · Oct 4, 1999 · N282WA · Boeing 727247 · Wing Spar
  > ONE FASTENER HOLE WAS MISDRILLED AND ELONGATED IN THE WING CENTER SECTION REAR SPAR WEB AT APPROXIMATELY LBL 41 DURING THE ACCOMPLISHMENT OF A MODIFICATION TO THE WEB. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 333636-14AD.
- [SDR DL72E992201](https://openairdocs.org/sdr/DL72E992201.md): Skin · corroded · Oct 4, 1999 · N282WA · Boeing 727247 · Wing, Plate/Skin
  > THE WING CENTER SECTION LOWER SKIN WAS FOUND CORRODED AT FS 820 AND RBL 13. THE DAMAGE WAS REPAIRED PER ERA 333611-14ADAT HMV.
- [SDR DL72E992200](https://openairdocs.org/sdr/DL72E992200.md): Skin · cracked · Oct 4, 1999 · N282WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > CRACK INDICATIONS WERE FOUND IN THE FUSELAGE SKIN LAP AT STRINGER 4L BETWEEN FS 360 AND FS 481. THE DAMAGE WAS REPAIRED PER ERA 333599-14AD AT HMV.
- [SDR DL72E992199](https://openairdocs.org/sdr/DL72E992199.md): Doubler · torn · Oct 4, 1999 · N282WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE AFT LAV SERVICE PANEL DOUBLER WAS FOUND TORN DURING MODIFICATION PER EO 4-69078-3AD. THE DAMAGE WAS REPAIRED PER ERA 333642-14 AT HMV.
- [SDR DL72E992198](https://openairdocs.org/sdr/DL72E992198.md): Frame · cracked · Oct 4, 1999 · N282WA · Boeing 727247 · Fuselage Main, Frame
  > THE LT FS 783.95 OVERWING EXIT FRAME WAS FOUND CRACKED AT HMV. THE DAMAGE WAS REPAIRED PER ERA 333610-14AD.
- [SDR DL72E992113](https://openairdocs.org/sdr/DL72E992113.md): Stringer · cracked · Sep 21, 1999 · N282WA · Boeing 727247 · Wing, Longeron/Stringer
  > THE LEFT WING STRINGER 17 WAS FOUND CRACKED AT WS 304. THE DAMAGE WAS REPAIRED PER ERA 333619-14 AT HMV.
- [SDR DL72E992074](https://openairdocs.org/sdr/DL72E992074.md): Track · corroded · Sep 16, 1999 · N282WA · Boeing 727247 · Trailing Edge Flaps
  > INB'D FLAP NR 5 FLAP TRACK, TYPICAL CORROSION AT MLG AND SPOILER BEAM ATTACH PADS AND WEAR AT FWD ATTACH LUGS, REF AD 90-07-05 AND 90-06-09. AUTHORIZED MACHINING OF ALL CORRODED AND WORN SURFACES. SPLICE PLATE REPAIR INSTALLED OVER OVERSIZED MLG BEAM ATTACH
- [SDR DL72E992073](https://openairdocs.org/sdr/DL72E992073.md): Track · corrosion · Sep 16, 1999 · N282WA · Boeing 727247 · Trailing Edge Flaps
  > INB'D FLAP, NR 4 FLAP TRACK: TYPICAL CORROSION AT MLG AND SPOILER BEAM ATTACH PADS AND TYPICAL WEAR AT FWD ATTACH LUGS AND SPACER BLOCK BOLT HOLES, REF AD 90-07-05 AND 90-06-09. AUTHORIZED MACHINING OF ALL CORROSION AND WEAR. SPLICE PLATE REPAIR INSTALLE
- [SDR DL72E992057](https://openairdocs.org/sdr/DL72E992057.md): Skin · cracked · Sep 15, 1999 · N282WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CRACKED AT THE STRINGER 4L LAP JOINT FROM FS 360-481. THE DAMAGE WAS REPAIRED PER ERA 333599-14AD AT HMV.
- [SDR DL72E992049](https://openairdocs.org/sdr/DL72E992049.md): Frame · cracked · Sep 14, 1999 · N282WA · Boeing 727247 · Fuselage Main, Frame
  > THE OVERWING EXIT FRAME AT FS 784 WAS FOUND CRACKED. THIS DAMAGE WAS REPAIRED AT HMV PER ERA 333610-14.
- [SDR DL72E992275](https://openairdocs.org/sdr/DL72E992275.md): Skin · worn · Sep 13, 1999 · N282WA · Boeing 727247 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE UPPER SKIN WAS FOUND WORN AT THE OUTBOARD END LEADING EDGE. THE SKIN WAS REPAIRED PER CMM 57052-0, FIG 803, BY CUTTING OUT THE DAMAGE AND INSTALLING A DOUBLER AND FILLER.
- [SDR DL72E992184](https://openairdocs.org/sdr/DL72E992184.md): Stringer · cracked · Sep 9, 1999 · N282WA · Boeing 727247 · Wing, Longeron/Stringer
  > AT HMV2, FOUND STRINGER TO RIB CRACKED AT ATTACHMENT HOLES WS 629.0 STR NR 3 MARKED. REMOVED FUEL PROBE REMOVED CLAMPS DISCONTINUED FUEL DUMPD, DRILLED REPAIR MM 57-13-0 FIG 802. INSTALLED REPAIR PER M/M 57-13-0 PG 802, RECONTED CLAMPS AND TUBE.
- [SDR DL72E992138](https://openairdocs.org/sdr/DL72E992138.md): Stringer · cracked · Sep 9, 1999 · N282WA · Boeing 727247 · Wing, Longeron/Stringer
  > AT HMV2, FOUND HFEL SHOWS CRACK INDICATION WS 656.5 STRINGER TO RIB UPPER FASTENER HOLE FWD MOST RIB. STOP DRILLED CRACK, DRILLED UP REPAIR PER MM 57-13-00 FIG 804, ANGLES FWD/AFT, INSTALLED ALL EXCEPT COVER PLATE PER MM 57-13-00. REPAIRED PER MM 57-13-00 FI
- [SDR DL72E992124](https://openairdocs.org/sdr/DL72E992124.md): Stringer · cracked · Sep 9, 1999 · N282WA · Boeing 727247 · Wing, Longeron/Stringer
  > FOUND AT HMV, HFEC SHOWS CRACK INDICATION: R/W STR TO RIB UPPER FWD FASTENER HOLE MARKED NR 7 AT WS 601-5. CUTOUT HOLE PER MM 57-13-0, DRILLED REPAIR ANGLE PER, DISCONNECTED FUEL TRANS TUBE, INSTALLED PARTS, REINSTALLED COVER CONT N/R 1282, RESTALLED TUBE, SE
- [SDR DL72E992185](https://openairdocs.org/sdr/DL72E992185.md): Rib · cracked · Sep 8, 1999 · N282WA · Boeing 727247 · Leading Edge Devices
  > AT HMV2, RIB CRACKED NR 7 L/E SLAT, NR 5 L/E SUPPORT RIB IS CRACKED AT UPPER LEG. REMOVED FASTENERS AND CLIPS, STOP DRILLED CRACK MM 57-54-00 FIG 809. REPAIRED PARTS PER SAME, INSTALLED DOUBLER PER 57-54-00.
- [SDR DL72E992172](https://openairdocs.org/sdr/DL72E992172.md): Rib · cracked · Sep 8, 1999 · N282WA · Boeing 727247 · Leading Edge Devices
  > AT HMV2, FOUND NR 4 L/E SUPPORT RIB IS CRACKED UPPER LEG. REMOVED FASTENERS AND CLIP, STOP DRILLED, FABRICATED DOUBLER REPAIR PER 57-54-00 FIG 809, AND INSTALLED PER SAME.
- [SDR DL72E992150](https://openairdocs.org/sdr/DL72E992150.md): Skin · cracked · Sep 8, 1999 · N282WA · Boeing 727247 · Leading Edge Devices
  > SKIN CRACKED UNDER FENCE NR 5 SLAT. REPAIRED AS PER MM 57-54-0.
- [SDR DL72E992139](https://openairdocs.org/sdr/DL72E992139.md): Actuator · loose · Sep 8, 1999 · N282WA · Boeing 727247 · Drag Control Actuator
  > AT HV2, FOUND NR 13 SPOILER ACTUATOR MOUNT BOX IS LOOSE AT LOWER MOUNT BOLTS 2, I/B MOUNT POINT IS MISSING SHIMS. SHIMS REPAIRED PER MM 57-42-0.
- [SDR DL72E992043](https://openairdocs.org/sdr/DL72E992043.md): Angle · cracked · Sep 7, 1999 · N282WA · Boeing 727247 · Wing Miscellaneous Structure
  > AT HMV, FOUND RT WING REAR SPAR LWR CHORD ANGLE IS CRACKED, O/B OF NR 5 FLAP TRACK. REMOVED CRACKED SECTION, FABRICATED NEW PER MM 57-55-0, AND INSTALLED.
- [SDR DL72E992153](https://openairdocs.org/sdr/DL72E992153.md): Spar · cracked · Sep 3, 1999 · N282WA · Boeing 727247 · Wing, Longeron/Stringer
  > LOWER SPAR CRACKED AT NUT PLATE ON NR 11 RIB, MARKED. REPAIRED PER M/M 57-54-0.
- [SDR DL72E992152](https://openairdocs.org/sdr/DL72E992152.md): Skin · cracked · Sep 3, 1999 · N282WA · Boeing 727247 · Wing, Plate/Skin
  > SKIN CRACKED AND WORN SEVERAL PLACES AT FENCE MOUNT AREA. REPAIRED PER M/M 57-54-0.
- [SDR DL72E991562](https://openairdocs.org/sdr/DL72E991562.md): Skin · cracked · Jul 10, 1999 · N282WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, FS 481-681, STRG 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 28 CRACKS ALONG
- [SDR DL72E991543](https://openairdocs.org/sdr/DL72E991543.md): Skin · cracked · Jul 9, 1999 · N282WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BETWEEN FS 440 & 460. THE CRACK WAS ROUTED OUT OF THE SKIN LAP AND AN EXT
- [SDR DL72E991283](https://openairdocs.org/sdr/DL72E991283.md): Rib · cracked · Jun 7, 1999 · N282WA · Boeing 727247 · Leading Edge Slat Actuator
  > A-1 LTR CHK, NR 5 SLAT ACT NOSE RIB CRACKED O/B SIDE AT FWD RADIUS.
- [SDR DL72E990969](https://openairdocs.org/sdr/DL72E990969.md): Fan · failed · May 3, 1999 · N282WA · Boeing 727247 · Air Distribution Fan
  > SMELL OF SMOKE NOTED IN CABIN PRIOR TO TAKEOFF. RETURNED TO GATE, GASPER FAN C/B POPPED. REPLACED GASPER FAN, OPS CKS OK. FAN HAD CAUSED SMOKE IN CABIN.
- [SDR DL72E990800](https://openairdocs.org/sdr/DL72E990800.md): Wire · failed · Apr 12, 1999 · N282WA · Boeing 727247 · Light System Wiring
  > A/C ESCAPE PATH LIGHTING FOUND INOP IN SEVERAL LOCATIONS. REPAIRED AND REPLACED GROUND WIRING AT THE FWD BATTERY PACK MULTI SPLICE AREA. ALL CK'S OK.
- [SDR DL72E990306](https://openairdocs.org/sdr/DL72E990306.md): Skin · punctured · Feb 14, 1999 · N282WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FS 520-540, STRINGER 25L-26L, REPAIR FOR PUNCTURE. THE FUSELAGE SKIN BETWEEN FS 520 AND 540 AND BETWEEN STRINGERS 25L AND 26L WAS PUNCTURED. THE DAMAGED SKIN WAS CLEANED UP WITH A 9 BY 5 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMI
- [SDR DL72E980765](https://openairdocs.org/sdr/DL72E980765.md): Oil Press Valve · failed · Apr 7, 1998 · N282WA · Boeing 727247 · Engine Oil Pressure
  > ON CLIMBOUT, NR 3 ENG OIL PRESS INDICATED IN THE RED, AT IDLE OIL PRESS IN THE GREEN. ANY ATTEMPT TO GO OVER 55 PERCENT. PRESSURE WOULD CLIMB TOWARDS THE RED. REPLACED OIL PRESSURE RELIEF VALVE.
- [SDR DL72E980743](https://openairdocs.org/sdr/DL72E980743.md): Channel · cracked · Apr 2, 1998 · N282WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > THE AFT CHANNEL OF THE VENTRAL STAIRWAY TORQUE BOX AT FS 1263 WAS FOUND WITH A TYPICAL CRACK. THE DAMAGED PART WAS REMOVED AND REPLACED WITH A NEW PART PER THE REQUIREMENTS OF BAC S/B 727-53-0129 AND DOCUMENTED PER ER/A 364426-14AD.
- [SDR DL72E980710](https://openairdocs.org/sdr/DL72E980710.md): Stiffener · cracked · Apr 1, 1998 · N282WA · Boeing 727247 · Leading Edge Devices
  > A 2 INCH CRACK WING L/E VERT STIFFENER AFT OF NR 3 SLAT I/B TRACK. REPAIRED PER MM 57-20-21 PG 813.
- [SDR DL72E980709](https://openairdocs.org/sdr/DL72E980709.md): Rib · worn · Apr 1, 1998 · N282WA · Boeing 727247 · Nacelle/Pylon, Frame/Spar/Rib
  > HOLE WORN THROUGH LIP OF NR 2 ENGINE CUTOUT AT 9 O'CLOCK POSITION. FOUND ON LETTER CHECK F-1. INSTALLED DOUBLER PER M/M 53-11-0 PG 801.
- [SDR DL72E980707](https://openairdocs.org/sdr/DL72E980707.md): Web · cracked · Apr 1, 1998 · N282WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND ON F1 LETTER CK,.125 INCH CRACK AT LIGHTENING HOLE IN LT TORQUE BOX VERTICLE WEB STA 1223. ROUTED OUT DAMAGED AREA PER MM 53-11-0.
- [SDR DL72E971195](https://openairdocs.org/sdr/DL72E971195.md): Heat Valve · failed · Jun 19, 1997 · N282WA · Boeing 727247 · Cabin Cooling System
  > UNABLE TO MAINTAIN CABIN PRESS ON CLIMBOUT WITH ONE PACK. ON MCO CABIN ROSE TO 7,000 FT WITH.18 DIFFERENTIAL BEFORE DESCENT TO REGAIN CONTROL. CARGO HEAT AND OUT FLOW VLV TRIED MANUALLY AS WELL. REPLACED CARGO HEAT VLV.
- [SDR DL72E970192](https://openairdocs.org/sdr/DL72E970192.md): Tie Bolt · sheared · Jan 8, 1997 · N282WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > THE INBOARD TENSION TIE BOLT AT THE RT S-3A WAS FOUND SHEARED. THIS PROBLEM IS THE SUBJECT OF BACO S/B 727-53-0178, REV 2. THE BOLT WAS REPLACED AND THE TENSION TIE FITTING WAS INSPECTED IN ACCORDANCE WITH THE SERVICE BULLETIN.
- [SDR DL72E970031](https://openairdocs.org/sdr/DL72E970031.md): Bracket · cracked · Jan 7, 1997 · N282WA · Boeing 727247 · Leading Edge Devices
  > FOUND ON E1 LETTER CK, NR 1 L/E FLAP ACTUATOR O/B MOUNT BRACKET CRACKED. REPAIRED PER M/M 57-20-21.
- [SDR DL72E970030](https://openairdocs.org/sdr/DL72E970030.md): Web · cracked · Jan 7, 1997 · N282WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > LOWER TORQUE BOX WEB CRACKED.25 INCH AT LIGHTENING HOLE STA 1223 RT. REPAIRED PER M/M 53-10-0.
- [SDR DL72E962430](https://openairdocs.org/sdr/DL72E962430.md): Light · inoperative · Oct 31, 1996 · N282WA · Boeing 727247 · Emergency Lighting
  > FOUND EMERGENCY EXIT LIGHT ABOVE 1L DOOR WILL NOT COME ON. REPLACED LIGHT EXIT ASSY.
- [SDR DL72E961711](https://openairdocs.org/sdr/DL72E961711.md): Spar Web · damaged · Jun 25, 1996 · N282WA · Boeing 727247 · Leading Edge Devices
  > UPPER SPAR WEB FLANGE DAMAGED BY STOP DRILLING RIBS NR 11 AND NR 12. MANUFACTURED DOUBLER, REPAIRED PER SRM 57-50-3 FIG 4.

Next page: https://openairdocs.org/deregistered/N282WA-2017-03-10/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N282WA' AND deregistration_id = 'N282WA-2017-03-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N282WA-2017-03-10/reports

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